View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57479U 26144.59175339 +.00000000 +00000-0 +00000-0 0 00004
2 57479 0.0179 308.8009 0001283 121.5371 289.6758 1.00270365 02
| Epoch (UTC): | 24 May 2026 14:12:07 |
| Eccentricity: | 0.0001283 |
| inclination: | 0.0179° |
| perigee height: | 35782 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 308.8009° |
| argument of perigee: | 121.5371° |
| revolutions per day: | 1.00270365 |
| mean anomaly at epoch: | 289.6758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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